Estimating formation stresses using radial profiles of three shear moduli

ABSTRACT

Maximum and minimum horizontal stresses, and horizontal to overburden stress ratio, are estimated using radial profiles of shear moduli. Inversion enables estimation of maximum and minimum horizontal stresses using radial profiles of three shear moduli associated with an orthogonal set of axes defined by the three principal stress directions. Differences in the far-field shear moduli are inverted together with two difference equations obtained from the radial profiles of the dipole shear moduli C44 and C55, and borehole stresses in the near-wellbore region. The horizontal to overburden stress ratio is estimated using differences in the compressional, dipole shear, and Stoneley shear slownesses at two depths in the same lithology interval where the formation exhibits azimuthal isotropy in cross-dipole dispersions, implying that horizontal stresses are nearly the same at all azimuths. The overburden to horizontal stress ratio in a formation with axial heterogeneity may also be estimated using the far-field Stoneley shear modulus C66 and dipole shear modulus C55 together with the radial variation of the dipole shear modulus C55 caused by near-wellbore stress concentrations.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a divisional application and claims the benefit under 35 U.S.C. § 120 to U.S. application Ser. No. 12/179,300 filed Jul. 24, 2008, which is incorporated by reference herein in its entirety.

FIELD OF THE INVENTION

The invention is generally related to analysis of subterranean formations, and more particularly to estimating formation stresses using radial profiles of three shear moduli.

BACKGROUND OF THE INVENTION

Formation stresses can affect geophysical prospecting and development of oil and gas reservoirs. For example, overburden stress, maximum and minimum horizontal stresses, pore pressure, wellbore pressure and rock strength can be used to produce a failure model to aid in well planning, wellbore stability calculations and reservoir management. It is known that elastic wave velocities change as a function of prestress in a propagating medium. For example, sonic velocities in porous rocks change as a function of effective prestress. However, estimating formation stresses based on velocity can be problematic because of influences on the horizontal shear modulus C₆₆. For example, the horizontal shear modulus C₆₆ is reduced in the presence of horizontal fluid mobility in a porous reservoir. Generally, the tube wave slowness decreases by about 2 to 3% in the presence of fluid mobility, resulting in a decrease in C₆₆ by about 4 to 6%. Conversely, the horizontal shear modulus C₆₆ is increased in the presence of high clay content in a shale interval. Consequently, it is difficult to accurately estimate the ratio of vertical to horizontal stress ratios without compensating for the changes in C₆₆.

Various devices are known for measuring formation characteristics based on sonic data. Mechanical disturbances are used to establish elastic waves in earth formations surrounding a borehole, and properties of the waves are measured to obtain information about the formations through which the waves have propagated. For example, compressional, shear and Stoneley wave information, such as velocity (or its reciprocal, slowness) in the formation and in the borehole can help in evaluation and production of hydrocarbon resources. One example of a sonic logging device is the Sonic Scanner® from Schlumberger. Another example is described in Pistre et al., “A modular wireline sonic tool for measurements of 3D (azimuthal, radial, and axial) formation acoustic properties, by Pistre, V., Kinoshita, T., Endo, T., Schilling, K., Pabon, J., Sinha, B., Plona, T., Ikegami, T., and Johnson, D.”, Proceedings of the 46^(th) Annual Logging Symposium, Society of Professional Well Log Analysts, Paper P, 2005. Other tools are also known. These tools may provide compressional slowness, Δt_(c), shear slowness, Δt_(s), and Stoneley slowness, Δt_(st), each as a function of depth, z, where slowness is the reciprocal of velocity and corresponds to the interval transit time typically measured by sonic logging tools. An acoustic source in a fluid-filled borehole generates headwaves as well as relatively stronger borehole-guided modes. A standard sonic measurement system uses a piezoelectric source and hydrophone receivers situated inside the fluid-filled borehole. The piezoelectric source is configured as either a monopole or a dipole source. The source bandwidth typically ranges from a 0.5 to 20 kHz. A monopole source primarily generates the lowest-order axisymmetric mode, also referred to as the Stoneley mode, together with compressional and shear headwaves. In contrast, a dipole source primarily excites the lowest-order flexural borehole mode together with compressional and shear headwaves. The headwaves are caused by the coupling of the transmitted acoustic energy to plane waves in the formation that propagate along the borehole axis. An incident compressional wave in the borehole fluid produces critically refracted compressional waves in the formation. Those refracted along the borehole surface are known as compressional headwaves. The critical incidence angle θ_(i)=sin⁻¹(V_(f)/V_(c)), where V_(f) is the compressional wave speed in the borehole fluid; and V_(c) is the compressional wave speed in the formation. As the compressional headwave travels along the interface, it radiates energy back into the fluid that can be detected by hydrophone receivers placed in the fluid-filled borehole. In fast formations, the shear headwave can be similarly excited by a compressional wave at the critical incidence angle θ_(i)=sin⁻¹(V_(f)/V_(s)), where V_(s) is the shear wave speed in the formation. It is also worth noting that headwaves are excited only when the wavelength of the incident wave is smaller than the borehole diameter so that the boundary can be effectively treated as a planar interface. In a homogeneous and isotropic model of fast formations, as above noted, compressional and shear headwaves can be generated by a monopole source placed in a fluid-filled borehole for determining the formation compressional and shear wave speeds. It is known that refracted shear headwaves cannot be detected in slow formations (where the shear wave velocity is less than the borehole-fluid compressional velocity) with receivers placed in the borehole fluid. In slow formations, formation shear velocities are obtained from the low-frequency asymptote of flexural dispersion. There are standard processing techniques for the estimation of formation shear velocities in either fast or slow formations from an array of recorded dipole waveforms. A different type of tool described in U.S. Pat. No. 6,611,761, issued Aug. 26, 2003 for “Sonic Well Logging for Radial Profiling” obtains radial profiles of fast and slow shear slownesses using the measured dipole dispersions in the two orthogonal directions that are characterized by the shear moduli c₄₄ and c₅₅ for a borehole parallel to the X₃-axis in an orthorhombic formation.

SUMMARY OF THE INVENTION

In accordance with an embodiment of the invention, a method for estimating stress in a formation in which a borehole is present comprises: determining radial profiles of Stoneley, fast dipole shear and slow dipole shear slownesses; estimating maximum and minimum horizontal stresses by inverting differences in far-field shear moduli with difference equations obtained from radial profiles of dipole shear moduli C44 and C55, and borehole stresses proximate to the borehole; and producing an indication of the maximum and minimum horizontal stresses in tangible form.

In accordance with another embodiment of the invention, apparatus for estimating stress in a formation in which a borehole is present comprises: at least one acoustic sensor that provides radial profiles of Stoneley, fast dipole shear and slow dipole shear slownesses; processing circuitry that estimates maximum and minimum horizontal stresses by inverting differences in far-field shear moduli with difference equations obtained from radial profiles of dipole shear moduli C₄₄ and C₅₅, and borehole stresses proximate to the borehole; and an output that produces an indication of the maximum and minimum horizontal stresses in tangible form.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1 is a schematic diagram of a borehole in a formation subject to the far-field principal stresses.

FIG. 2 is a schematic diagram of a borehole of radius “a” subject to formation stresses in a poroelastic formation with pore pressure P_(P) and wellbore pressure P_(W).

FIG. 3 illustrates a logging tool for estimating formation stresses using radial profiles of three shear moduli.

FIG. 4 is a flow diagram illustrating steps of a method in accordance with an embodiment of the invention.

FIG. 5 illustrates radial variation of axial (σZZ), hoop (σθθ), and radial (σrr) effective stresses at an azimuth parallel to the maximum horizontal stress direction at a given depth.

FIG. 6 illustrates radial variation of axial (σZZ), hoop (σθθ), and radial (σrr) effective stresses at an azimuth perpendicular to the maximum horizontal stress direction.

FIG. 7 illustrates fast and slow shear dispersion curves which exhibit a crossing signature together with the lowest-order axisymmetric Stoneley dispersion

FIG. 8 illustrates fast and slow shear dispersion curves which do not exhibit a crossing signature, and the fast and slow dipole dispersions essentially overlay implying that SHmax=Shmin.

FIG. 9 illustrates an algorithm for solving for the unknowns Ae and σH/σ V, which enables determination of SH, and an acoustoelastic coefficient Ae.

DETAILED DESCRIPTION

Embodiments of the invention will be described with reference to principal stresses illustrated in FIG. 1, and triaxial stresses Txx, Tyy, and Tzz, together with wellbore pressure Pw, and pore pressure Pp as illustrated in FIG. 2. The borehole radius is denoted by “a.” As previously discussed, sonic velocities, and therefore slownesses, are sensitive to effective stresses in the propagating medium. Effective stress σ_(ij)=T_(ij)−δ_(ij)P_(P), where T_(ij) is the applied stress, δ_(ij) is the Kronecker delta, and P_(P) is the pore pressure.

FIG. 3 illustrates one example of a logging tool (106) used to acquire and analyze data in accordance with an embodiment of the invention. The tool has a plurality of receivers and transmitters. The illustrated logging tool (106) also includes multi-pole transmitters such as crossed dipole transmitters (120, 122) (only one end of dipole (120) is visible in FIG. 1) and monopole transmitters (109) (close) and (124) (far) capable of exciting compressional, shear, Stoneley, and flexural waves. The logging tool (106) also includes receivers (126), which are spaced apart some distance from the transmitters. Each receiver may include multiple hydrophones mounted azimuthally at regular intervals around the circumference of the tool. Other configurations, such as a Digital Sonic Imaging (DSI) tool with four receivers at each of eight receiver stations, or incorporating other multi-pole sources such as quadrupole, are also possible. The use of a plurality of receivers and transmitters results in improved signal quality and adequate extraction of the various borehole signals over a wide frequency band However, the distances, number and types of receivers and transmitters shown in this embodiment are merely one possible configuration, and should not be construed as limiting the invention.

The subsurface formation (102) is traversed by a borehole (104) which may be filled with drilling fluid or mud. The logging tool (106) is suspended from an armored cable (108) and may have optional centralizers (not shown). The cable (108) extends from the borehole (104) over a sheave wheel (110) on a derrick (112) to a winch forming part of surface equipment, which may include an analyzer unit (114). Well known depth gauging equipment (not shown) may be provided to measure cable displacement over the sheave wheel (110). The tool (106) may include any of many well known devices to produce a signal indicating tool orientation. Processing and interface circuitry within the tool (106) amplifies, samples and digitizes the tool's information signals for transmission and communicates them to the analyzer unit (114) via the cable (108). Electrical power and control signals for coordinating operation of the tool (106) may be generated by the analyzer unit (114) or some other device, and communicated via the cable (108) to circuitry provided within the tool (106). The surface equipment includes a processor subsystem (116) (which may include a microprocessor, memory, clock and timing, and input/output functions—not separately shown), standard peripheral equipment (not separately shown), and a recorder (118).

FIG. 4 is a flow diagram that illustrates a method of estimating formation stresses using radial profiles of three shear moduli. If practical, a depth interval characterized by relatively uniform lithology is selected for evaluation of stresses. Monopole and cross-dipole sonic data is then obtained with the tool (106, FIG. 3) over the selected interval, as indicated by step (400). The monopole and cross-dipole data, density (ρ_(f),) far field velocity (V_(f)), and borehole radius (a) are used to determine radial profiles of Stoneley, fast dipole shear slowness and slow dipole shear slowness as indicated by step (402). Formation bulk density (ρ_(b)) obtained in step (404) is then used to calculate radial profiles of the three shear moduli (C44, C55, C66) as shown in step (406). The next step is selected based on the result of the shear moduli calculation.

Prior to describing selection of the next step, the effects of borehole presence in a formation will be explained with reference to FIGS. 5 and 6. The presence of a borehole causes near-wellbore stress distributions that can be described by the following equations (Jaeger and Cook, 1969)

$\begin{matrix} {{\sigma_{r\; r} = {{\frac{\left( {\sigma_{H} + \sigma_{h}} \right)}{2}\left( {1 - \frac{a^{2\;}}{r}} \right)} + {\frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}\left( {1 - \frac{4a^{2}}{r^{2}} + \frac{3a^{4}}{r^{4}}} \right)\cos\; 2\theta} - {P_{W}\frac{a^{2}}{r^{2}}}}},} & (1) \\ {{\sigma_{\theta\theta} = {{\frac{\left( {\sigma_{H} + \sigma_{h}} \right)}{2}\left( {1 - \frac{a^{2}}{r^{2}}} \right)} - {\frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}\left( {1 + \frac{3a^{4}}{r^{4}}} \right)\cos\; 2\theta} + {P_{W}\frac{a^{2}}{r^{2}}}}},} & (2) \\ {\mspace{79mu}{{\sigma_{r\;\theta} = {{- \frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}}\left( {1 + \frac{2a^{2}}{r^{2}} - \frac{3a^{4}}{r^{4}}} \right)\sin\; 2\theta}},}} & (3) \\ {\mspace{79mu}{{\sigma_{Z\; Z} = {\sigma_{V} - {v\frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}\frac{2a^{2}}{r^{2}}\cos\; 2\theta}}},}} & (4) \end{matrix}$ where σ_(rr), σ_(θθ), σ_(rθ), and σ_(ZZ) denote the effective radial, hoop, radial-shear, and axial stresses, respectively; σ_(V), σ_(H), and σ_(h) represent the effective far-field overburden, maximum horizontal, minimum horizontal stresses, respectively; and “a” denotes the borehole radius, and θ is the azimuth measured from the maximum horizontal stress direction. In the absence of a borehole, the far-field stresses are given by:

$\begin{matrix} {{\sigma_{r\; r} = {\frac{\left( {\sigma_{H} + \sigma_{h}} \right)}{2} + {\frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}\cos\; 2\theta}}},} & (5) \\ {{\sigma_{\theta\theta} = {\frac{\left( {\sigma_{H} + \sigma_{h}} \right)}{2} - {\frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}\cos\; 2\theta}}},} & (6) \\ {{\sigma_{r\;\theta} = {{- \frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}}\sin\; 2\theta}},{and}} & (7) \\ {\sigma_{Z\; Z} = {\sigma_{V}.}} & (8) \end{matrix}$ Subtracting the far-field stresses from the near-wellbore stresses yields incremental stresses as the borehole surface is approached as follows:

$\begin{matrix} {{{\Delta\sigma}_{rr} = {{\frac{\left( {\sigma_{H} + \sigma_{h}} \right)}{2}\left( \frac{a^{2\;}}{r^{2}} \right)} - {\frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}\left( {\frac{4a^{2}}{r^{2}} - \frac{3a^{4}}{r^{4}}} \right)\cos\; 2\theta} - {P_{W}\frac{a^{2}}{r^{2}}}}},} & (9) \\ {{{\Delta\sigma}_{\theta\theta} = {{\frac{\left( {\sigma_{H} + \sigma_{h}} \right)}{2}\left( \frac{a^{2}}{r^{2}} \right)} + {\frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}\left( \frac{3a^{4}}{r^{4}} \right)\cos\; 2\theta} + {P_{W}\frac{a^{2}}{r^{2}}}}},} & (10) \\ {\mspace{79mu}{{\sigma_{r\;\theta} = {{- \frac{\left( {\sigma_{H} - \sigma_{h}} \right)}{2}}\left( {\frac{2a^{2}}{r^{2}} - \frac{3a^{4}}{r^{4}}} \right)\sin\; 2\theta}},}} & (11) \\ {\mspace{79mu}{{\sigma_{Z\; Z} = {{- {v\left( {\sigma_{H} - \sigma_{h}} \right)}}\left( \frac{2a^{2}}{r^{2}} \right)\cos\; 2\theta}},}} & (12) \end{matrix}$ where P_(W) denotes the wellbore pressure at a given depth.

In the case of an isotropically loaded reference state, shear moduli in the three orthogonal planes are the same, i.e., C₄₄=C₅₅=C₆₆=μ. When this type of formation is subject to anisotropic incremental stresses, changes in the shear moduli can be expressed as

$\begin{matrix} {{{\Delta\; C_{55}} = {{\left\lbrack {C_{55} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{11}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {C_{144} - {\left( {1 + {2v}} \right)C_{55}} - {2v\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{22}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{2{\mu\left( {1 + v} \right)}} + C_{55} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{33}}{2{\mu\left( {1 + v} \right)}}}}},} & (13) \end{matrix}$ where ΔC₅₅ is obtained from the fast-dipole shear slowness from sonic data acquired by a dipole transmitter aligned parallel to the X₁-direction and borehole parallel to the X₃-direction; the quantities C₅₅, μ, and v are the linear elastic moduli, whereas C₁₄₄ and C₁₅₅ are the formation nonlinear constants in the chosen reference state; and Δσ₃₃, Δσ₁₁, and Δσ₂₂, respectively, denote the effective overburden (parallel to the X₃-direction), maximum horizontal (parallel to the X₁-direction), and minimum horizontal (parallel to the X₂-direction) stresses at a chosen depth of interest,

$\begin{matrix} {{{\Delta\; C_{44}} = {{\left\lbrack {{{- \left( {1 + {2v}} \right)}C_{44}} + C_{144} - {2v\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{11}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{{- v}\; C_{144}} + C_{44} + {\left( {1 - v} \right)\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{22}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{2{\mu\left( {1 + v} \right)}} + C_{44} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{33}}{2{\mu\left( {1 + v} \right)}}}}},} & (14) \end{matrix}$ where ΔC₄₄ is obtained from the slow-dipole shear slowness from sonic data acquired by a dipole transmitter aligned parallel to the X₂-direction and borehole parallel to the X₃-direction;

$\begin{matrix} {{{\Delta\; C_{66}} = {{\left\lbrack {{\mu\left( {1 + v} \right)} + C_{66} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{{- \left( {1 + {2v}} \right)}\; C_{66}} + C_{144} - {2v\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{33}}{2{\mu\left( {1 + v} \right)}}}}},} & (15) \end{matrix}$ where ΔC₆₆ is obtained from the Stoneley shear slowness dispersion from sonic data acquired by a monopole transmitter at a chosen depth of interest.

Referring to FIGS. 4 and 7, in the case where the fast and slow shear dispersion curves exhibit a crossing signature, step (408) is used. Step (408) includes two component calculations that are made with the aid of overburden stress (S_(V)), wellbore pressure (P_(W)), pore pressure (P_(P)), Biot coefficient α, and borehole radius (a) data, obtained in step (410). A first component calculation is to form two difference equations using the far-field shear moduli C44, C55, and C66. A second component calculation is to form two difference equations using [C55(r/a=6)−C55(r/a=2)] and [C44(r/a=6)−C55(r/a=2)]. Assuming that the X₁-, X₂-, and X₃-axes, respectively, are parallel to the maximum horizontal (σ_(H)), minimum horizontal (σ_(h)), and vertical (σ_(V)) stresses, equations (13)-(15) yield difference equations in the effective shear moduli in terms of differences in the principal stress magnitudes through an acoustoelastic coefficient defined in terms of formation nonlinear constants referred to a chosen reference state and for a given formation lithology. The following three equations relate changes in the shear moduli to corresponding changes in the effective principal stresses in a homogeneously stressed formation as would be the case in the far-field, sufficiently away from the borehole surface: ΔC ₄₄ −ΔC ₆₆ =A _(E)(Δσ₃₃−Δσ₁₁),  (16) ΔC ₅₅ −ΔC ₆₆ =A _(E)(Δσ₃₃−Δσ₂₂),  (17) ΔC ₄₄ −ΔC ₄₄ =A _(E)(Δσ₁₁−Δσ₂₂),  (18) where Δσ₃₃, Δσ₁, and Δσ₂₂ denote changes in the effective overburden, maximum horizontal, and minimum horizontal stresses, respectively; and

$\begin{matrix} {{A_{E} = {2 + \frac{C_{456}}{\mu}}},} & (19) \end{matrix}$ is the acoustoelastic coefficient, C₅₅ and C₄₄ denote the shear moduli for the fast and slow shear waves, respectively; C₄₅₆=(C₁₅₅−C₁₄₄)/2, is a formation nonlinear parameter that defines the acoustoelastic coefficient; and μ represents the shear modulus in a chosen reference state. However, only two of the three difference equations (16), (17), and (18) are independent. The presence of differential stress in the cross-sectional plane of the borehole causes dipole shear wave splitting and the observed shear slowness anisotropy can be used to calculate the acoustoelastic coefficient A_(E) from equation (18), provided estimates of the three principal stresses as a function of depth are available. Note that the dipole shear waves are largely unaffected by the fluid mobility. The stress-induced change in the Stoneley shear modulus C₆₆ is then calculated using equations (16) and (17), and the effective stress magnitudes Δσ_(V), Δσ_(H), and Δσ_(h) at a given depth are obtained.

The next step (412) is to use an algorithm to solve for the unknowns. Combining the two difference equations (16) and (17) in terms of the far-field shear moduli yields four independent equations to solve for the four unknowns—Δσ_(H), Δσ_(h), C₁₄₄ and C₁₅₅. Equations (13), (14), and (15) can be expressed in terms of the principal stress parameters Δσ_(E)', Δσ_(h), and Δσ_(V) as follows:

$\begin{matrix} {{{\Delta\; C_{55}} = {{\left\lbrack {C_{55} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{H}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {C_{144} - {\left( {1 + {2v}} \right)C_{55}} - {2v\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{h}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{2{\mu\left( {1 + v} \right)}} + C_{55} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{V}}{2{\mu\left( {1 + v} \right)}}}}},} & (20) \\ {{{\Delta\; C_{44}} = {{\left\lbrack {{{- \left( {1 + {2v}} \right)}C_{44}} + C_{144} - {2v\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{H}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{{- v}\; C_{144}} + C_{44} + {\left( {1 - v} \right)\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{h}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{2{\mu\left( {1 + v} \right)}} + C_{44} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{V}}{2{\mu\left( {1 + v} \right)}}}}},} & (21) \\ {{{\Delta\; C_{66}} = {{\left\lbrack {{\mu\left( {1 + v} \right)} + C_{66} - {v\; C_{144}} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{\left( {{\Delta\sigma}_{H} + {\Delta\sigma}_{h}} \right)}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{{- \left( {1 + {2v}} \right)}\; C_{66}} + C_{144} - {2v\; C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{V}}{2{\mu\left( {1 + v} \right)}}}}},} & (22) \end{matrix}$

-   Defining the following non-dimensional parameters

$\begin{matrix} {{S_{H} = \frac{\Delta\;\sigma_{H}}{2{\mu\left( {1 - v} \right)}}},{S_{h} = \frac{\Delta\;\sigma_{h}}{2{\mu\left( {1 - v} \right)}}},{S_{v} = \frac{\Delta\;\sigma_{v}}{2{\mu\left( {1 + v} \right)}}},{and}} & (23) \\ {{A_{1} = {{{- v}\; C_{144}} + {\left( {1 - v} \right)C_{155}}}},{A_{2} = {C_{144} - {2v\; C_{155}}}},} & (24) \end{matrix}$ it is possible to express the nonlinear constants C₁₄₄ and C₁₅₅ in terms of A₁ and A₂, and the acoustoelastic coefficient A_(E) can also be expressed in terms of A₁ and A₂ as shown below:

$\begin{matrix} {{C_{144} = \frac{{2v\; A_{1}} + {\left( {1 - v} \right)A_{2}}}{\left( {1 - {2v}} \right)\left( {1 + v} \right)}},{C_{155} = \frac{A_{1} + {v\; A_{2}}}{\left( {1 - {2v}} \right)\left( {1 + v} \right)}},} & (25) \\ {{{C_{155} - C_{144}} = \frac{A_{1} - A_{2}}{1 + v}},} & (26) \\ {{A_{E} = {{2 + {\frac{1}{2\mu}\left( {C_{155} - C_{144}} \right)}} = {2 + \frac{A_{1} - A_{2}}{2{\mu\left( {1 + v} \right)}}}}},} & (27) \\ {{{{\Delta\; C_{44}} - {\Delta\; C_{66}}} = {A_{E}\left( {{\Delta\;\sigma_{V}} - {\Delta\sigma}_{H}} \right)}},} & (28) \\ {{{\Delta\; C_{55}} - {\Delta\; C_{66}}} = {{A_{E}\left( {{\Delta\;\sigma_{V}} - {\Delta\sigma}_{h}} \right)}.}} & (29) \end{matrix}$ An expression for the stress ratio is obtained from equations (16) and (17)

$\begin{matrix} {\frac{\Delta\;\sigma_{h}}{\Delta\;\sigma_{V}} = {{1 - \frac{{\Delta\; C_{55}} - {\Delta\; C_{66}}}{{\Delta\; C_{44}} - {\Delta\; C_{66}}} + {\left( \frac{{\Delta\; C_{55}} - {\Delta\; C_{66}}}{{\Delta\; C_{44}} - {\Delta\; C_{66}}} \right)\frac{\Delta\;\sigma_{H}}{\Delta\;\sigma_{V}}}} = {\frac{{\Delta\; C_{44}} - {\Delta\; C_{55}}}{{\Delta\; C_{44}} - {\Delta\; C_{66}}} + {\left( \frac{{\Delta\; C_{55}} - {\Delta\; C_{66}}}{{\Delta\; C_{44}} - {\Delta\; C_{66}}} \right){\frac{\Delta\;\sigma_{H}}{{\Delta\sigma}_{V}}.}}}}} & \left. 30 \right) \end{matrix}$ Subtracting equation (28) from (29), and substituting for A_(E) from equation (27), yields

$\begin{matrix} {{{\Delta\; C_{55}} - {\Delta\; C_{44}}} = {\left\lbrack {{2{\mu\left( {1 - v} \right)}} + A_{1} - A_{2}} \right\rbrack{\frac{{\Delta\;\sigma_{H}} - {\Delta\;\sigma_{h}}}{2{\mu\left( {1 + v} \right)}}.}}} & (31) \end{matrix}$ This results in one of the two equations relating A₁ and A₂

$\begin{matrix} {{A_{1} - A_{2}} = {2{{{\mu\left( {1 - v} \right)}\left\lbrack {\frac{{\Delta\; C_{55}} - {\Delta\; C_{44}}}{{\Delta\;\sigma_{H}} - {\Delta\;\sigma_{h}}} - 1} \right\rbrack}.}}} & (32) \end{matrix}$ Different A₁ and A₂ values can be obtained for different Δσ_(H)/Δσ_(V) as follows

$\begin{matrix} {{{\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 6} \right)}} - {\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}}} = {{\left( {\mu + A_{1}} \right)\left\lbrack {{S_{H}^{\theta = 0}\left( {{r\text{/}a} = 6} \right)} - {S_{H}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}} \right\rbrack} + {\left( {{- {\mu\left( {1 + {2v}} \right)}} + A_{2}} \right)\left\lbrack {{S_{h}^{\theta = 0}\left( {{r\text{/}a} = 6} \right)} - {S_{h}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}} \right\rbrack} + {\left( {\mu + A_{1}} \right)\left\lbrack {{S_{v}^{\theta = 0}\left( {{r\text{/}a} = 6} \right)} - {S_{v}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}} \right\rbrack}}} & (33) \\ {\frac{{\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 6} \right)}} - {\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}}}{\Delta\;\sigma_{V}} = {{\left( {\mu + A_{1}} \right)\left\lbrack {{\xi_{1}^{H\; H}\frac{\sigma_{H}}{\sigma_{V}}} + {\xi_{2}^{H\; H}\frac{\sigma_{h}}{\sigma_{V}}} + {\xi_{3}^{H\; H}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack} + {\left( {{- {\mu\left( {1 + {2v}} \right)}} + A_{2}} \right)\left\lbrack {{\xi_{1}^{h\; h}\frac{\sigma_{H}}{\sigma_{V}}} + {\xi_{2}^{h\; h}\frac{\sigma_{h}}{\sigma_{V}}} + {\xi_{3}^{h\; h}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack} + {{\left( {\mu + A_{1}} \right)\left\lbrack {{\xi_{1}^{v\; v}\frac{\sigma_{H}}{\sigma_{V}}} + {\xi_{2}^{v\; v}\frac{\sigma_{h}}{\sigma_{V}}}} \right\rbrack}\mspace{14mu}{where}}}} & (34) \\ {\mspace{79mu}{{\xi_{1}^{H\; H} = {{- \frac{177}{2592}} + \frac{17}{32}}},\mspace{79mu}{\xi_{2}^{H\; H} = {\frac{105}{2592} + \frac{9}{32}}},\mspace{79mu}{\xi_{3}^{H\; H} = {{- \frac{1}{36}} + \frac{1}{4}}},\mspace{85mu}{\xi_{1}^{h\; h} = {\frac{33}{2592} - \frac{1}{32}}},\mspace{79mu}{\xi_{2}^{h\; h} = {\frac{39}{2592} - \frac{7}{32}}},\mspace{79mu}{\xi_{3}^{h\; h} = {\frac{1}{36} - \frac{1}{4}}},\mspace{79mu}{\xi_{1}^{V\; V} = {{- \frac{2}{36}} + \frac{1}{2}}},\mspace{79mu}{\xi_{2}^{V\; V} = {\frac{2}{36} - {\frac{1}{2}.}}}}} & (35) \end{matrix}$ Equation (34) can be rewritten in a compact form shown below

$\begin{matrix} {{\frac{X_{c}}{\Delta\;\sigma_{v}} = {{\left( {\mu + A_{1}} \right)\left( {S_{1} + S_{3}} \right)} + {\left( {{- {\mu\left( {1 - {2v}} \right)}} + A_{2}} \right)S_{2}}}},{where}} & (36) \\ {{X_{c} = {{\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 6} \right)}} - {\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}}}}{S_{1} = \left\lbrack {{\xi_{1}^{H\; H}\frac{\sigma_{H}}{\sigma_{V}}} + {\xi_{2}^{H\; H}\frac{\sigma_{h}}{\sigma_{V}}} + {\xi_{3}^{H\; H}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack}{{S_{2} = \left\lbrack {{\xi_{1}^{h\; h}\frac{\sigma_{H}}{\sigma_{V}}} + {\xi_{2}^{h\; h}\frac{\sigma_{h}}{\sigma_{V}}} + {\xi_{3}^{h\; h}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack},{S_{3} = \left\lbrack {{\xi_{1}^{v\; v}\frac{\sigma_{H}}{\sigma_{V}}} + {\xi_{2}^{v\; v}\frac{\sigma_{h}}{\sigma_{V}}}} \right\rbrack}}} & (37) \end{matrix}$ Similarly,

$\begin{matrix} \left. {{{\Delta\;{C_{44}^{\theta = 90}\left( {{r\text{/}a} = 6} \right)}} - {\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}}} = {{\left( {\mu + A_{1}} \right)\left\lbrack {{S_{H}^{\theta = 90}\left( {{r\text{/}a} = 6} \right)} - {S_{H}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}} \right\rbrack} + {\left( {{- {\mu\left( {1 + {2v}} \right)}} + A_{2}} \right)\left\lbrack {{S_{h}^{\theta = 90}\left( {{r\text{/}a} = 6} \right)} - {S_{h}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}} \right\rbrack} + {\left( {\mu + A_{1}} \right){S_{v}^{\theta = 90}\left( {{r\text{/}a} = 6} \right)}} - {S_{v}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}}} \right\rbrack & (38) \\ {\frac{{\Delta\;{C_{44}^{\theta = 90}\left( {{r\text{/}a} = 6} \right)}} - {\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}}}{\Delta\;\sigma_{V}} = {{\left( {\mu + A_{1}} \right)\left\lbrack {{\psi_{1}^{h\; H}\frac{\sigma_{H}}{\sigma_{V}}} + {\psi_{2}^{h\; H}\frac{\sigma_{h}}{\sigma_{V}}} + {\psi_{3}^{h\; H}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack} + {\left( {{- {\mu\left( {1 + {2v}} \right)}} + A_{2}} \right)\left\lbrack {{\psi_{1}^{H\; h}\frac{\sigma_{H}}{\sigma_{V}}} + {\psi_{2}^{H\; h}\frac{\sigma_{h}}{\sigma_{V}}} + {\psi_{3}^{H\; h}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack} + {{\left( {\mu + A_{1}} \right)\left\lbrack {{\psi_{1}^{v\; v}\frac{\sigma_{H}}{\sigma_{V}}} + {\psi_{2}^{v\; v}\frac{\sigma_{h}}{\sigma_{V}}}} \right\rbrack}\mspace{14mu}{where}}}} & (39) \\ {\mspace{79mu}{{\psi_{1}^{h\; H} = {{- \frac{105}{2592}} + \frac{17}{32}}},\mspace{79mu}{\psi_{2}^{h\; H} = {{- \frac{177}{2592}} - \frac{9}{32}}},\mspace{79mu}{\psi_{3}^{h\; H} = {{- \frac{1}{36}} + \frac{1}{4}}},\mspace{85mu}{\psi_{1}^{H\; h} = {\frac{39}{2592} - \frac{1}{32}}},\mspace{79mu}{\psi_{2}^{H\; h} = {\frac{33}{2592} - \frac{7}{32}}},\mspace{79mu}{\psi_{3}^{H\; h} = {\frac{1}{36} - \frac{1}{4}}},\mspace{79mu}{\psi_{1}^{V\; V} = {\frac{2}{36} + \frac{1}{2}}},\mspace{79mu}{\psi_{1}^{V\; V} = {{- \frac{2}{36}} - {\frac{1}{2}.}}}}} & (40) \end{matrix}$ Equation (39) can be rewritten in a compact form as follows:

$\begin{matrix} {{\frac{Y_{c}}{\Delta\;\sigma_{v}} = {{\left( {\mu + A_{1}} \right)\left( {S_{4} + S_{6}} \right)} + {\left( {{- {\mu\left( {1 + {2v}} \right)}} + A_{2}} \right)S_{5}}}},{where}} & (41) \\ {{Y_{c} = {{\Delta\;{C_{44}^{\theta = 90}\left( {{r\text{/}a} = 6} \right)}} - {\Delta\;{C_{55}^{\theta = 0}\left( {{r\text{/}a} = 2} \right)}}}}{{S_{4} = \left\lbrack {{\psi_{1}^{h\; H}\frac{\sigma_{H}}{\sigma_{V}}} + {\psi_{2}^{h\; H}\frac{\sigma_{h}}{\sigma_{V}}} + {\psi_{3}^{h\; H}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack},{S_{5} = \left\lbrack {{\psi_{1}^{H\; h}\frac{\sigma_{H}}{\sigma_{V}}} + {\psi_{2}^{H\; h}\frac{\sigma_{h}}{\sigma_{V}}} + {\psi_{3}^{H\; h}\frac{P_{W}}{\sigma_{V}}}} \right\rbrack},{S_{6} = {\left\lbrack {{\psi_{1}^{v\; v}\frac{\sigma_{H}}{\sigma_{V}}} + {\psi_{2}^{v\; v}\frac{\sigma_{h}}{\sigma_{V}}}} \right\rbrack.}}}} & (42) \end{matrix}$ Solving

$\begin{matrix} {{\frac{X_{c}}{\Delta\;\sigma_{v}} = {{\left( {\mu + A_{1}} \right)\left( {S_{1} + S_{3}} \right)} + {\left( {{- {\mu\left( {1 + {2v}} \right)}} + A_{2}} \right)S_{2}}}},} & (43) \\ {{\frac{Y_{c}}{\Delta\;\sigma_{v}} = {{\left( {\mu + A_{1}} \right)\left( {S_{4} + S_{6}} \right)} + {\left( {{- {\mu\left( {1 + {2v}} \right)}} + A_{2}} \right)S_{5}}}},} & (44) \end{matrix}$ for A₁ and A₂, yields

$\begin{matrix} {{A_{1} = \frac{{S_{2}G_{2}} - {S_{5}G_{1}}}{{S_{2}\left( {S_{4} + S_{6}} \right)} - {S_{5}\left( {S_{1} + S_{3}} \right)}}},} & (45) \\ {{A_{2} = \frac{{\left( {S_{4} + S_{6}} \right)G_{1}} - {\left( {S_{1} + S_{3}} \right)G_{2}}}{{S_{2}\left( {S_{4} + S_{6}} \right)} - {S_{5}\left( {S_{1} + S_{3}} \right)}}},{where}} & (46) \\ {{G_{1} = {\frac{X_{c}}{\Delta\;\sigma_{V}} + \left\lbrack {{- {\mu\left( {S_{1} + S_{3}} \right)}} + {{\mu\left( {1 + {2v}} \right)}S_{2}}} \right\rbrack}},} & (47) \\ {G_{2} = {\frac{Y_{c}}{\Delta\;\sigma_{V}} + {\left\lbrack {{- {\mu\left( {S_{4} + S_{6}} \right)}} + {{\mu\left( {1 + {2v}} \right)}S_{5}}} \right\rbrack.}}} & (48) \end{matrix}$

SHmax, Shmin, and an acoustoelastic coefficient Ae are calculated in step (414). The acoustoelastic parameter Ae is calculated as a function the stress ratio σ_(H)/σ_(V) using equation (28). σ_(h)/σ_(V) is calculated in terms of σ_(H)/σ_(V) using equation (30). True Ae is calculated in terms of C₅₅, C₄₄, σ_(H), and σ_(h) using equation (18). A1 and A2 are calculated from equations (45) and (46). Ae is again calculated from equation (27). The error ε=abs[(Ae−True Ae)/True Ae] is minimized as a function of σ_(H)/σ_(V). An estimated value of σ_(H)/σ_(V) is obtained when the error ε is minimum. σ_(h)/σ_(V) can then be calculated using equation (30). Pore pressure is then added to the estimated effective stresses to obtain absolute magnitude of formation stress magnitudes at the selected depth interval.

Referring back to step (406) and to FIGS. 4 and 8, in the case where the fast and slow shear dispersion curves do not exhibit a crossing signature, and the fast and slow dipole dispersions essentially overlay, step (416) is used. When the fast and slow dipole dispersions overlay, implying that there is no shear wave splitting for propagation along the borehole axis, it suggests that the maximum and minimum horizontal stresses (SHmax=Shmin) are nearly the same. Under these circumstances it is possible to estimate the ratio of the overburden stress Sv and the horizontal stress SH (SH=SHmax=Shmin) in a chosen depth interval with reasonably uniform lithology using the far-field sonic velocity (or slowness) gradients. Step (416) includes two component calculations for this particular case: Forming a difference equation using the far-field shear moduli C44(=C55), and C66; and forming another difference equation using [C55(r/a=6)−C55(r/a=2)]. An algorithm is then used to solve for the unknowns Ae and the effective stress ratio σ_(H)/σ_(V), as indicated by step (418), which enables determination of the horizontal stress magnitude SH, and an acoustoelastic coefficient Ae, as indicated by step (420).

FIG. 9 shows a workflow for implementing necessary corrections in the shear modulus C₆₆ in the presence of either fluid mobility in a reservoir or structural anisotropy in shales. Estimation of formation stress magnitudes (910) using the three shear moduli requires compensation (912) for fluid mobility effects in a reservoir and structural anisotropy effects in overburden or underburden shales as calculated in step (900).

When fluid mobility estimates are known from any of the techniques known in the art, such as measurements on a core sample, pressure transient analysis, or nuclear magnetic resonance data, it is possible to calculate mobility-induced decrease in the Stoneley shear modulus C₆₆ using a standard Biot model. Under this situation, the workflow increases the measured C₆₆ by the same amount before inverting the three shear moduli for formation stresses. In contrast, structural anisotropy effects in shales cause the Stoneley shear modulus C₆₆ to be larger than the dipole shear moduli C₄₄ or C₅₅. One way to compensate for the structural or intrinsic anisotropy effects, as indicated in step (902), is to measure shear velocities propagating parallel and perpendicular to the layer in a core sample subjected to a confining pressure and estimate the Thomsen anisotropy parameter γ. Insofar as the shale anisotropy increases the magnitude of C₆₆, we must decrease the measured C₆₆ by the same amount in step (904) before inverting the three shear moduli in step (906) for formation stress magnitudes.

One option (“Algorithm I”), is to estimate the horizontal to overburden stress ratio in a reasonably uniform depth interval using differences in the compressional and shear slownesses at two depths within the chosen interval. Another option (“Algorithm II”) is to estimate the horizontal to overburden stress ratio using the two far-field shear moduli (C₄₄ and C₆₆), and radial profile of the dipole shear modulus (C₄₄). This algorithm can be applied in depth intervals that are axially heterogeneous insofar as the difference equations use shear moduli at the same chosen depth.

Algorithm I will now be described. There are two sets of quantities that need to be estimated from the inversion of changes in sonic velocities caused primarily by formation stress changes. The first set involves determination of the three nonlinear constants, and the second set comprises the estimation of stress magnitudes. The acoustoelastic equations relating changes in the sonic velocities caused by changes in stresses in the propagating medium contain product of unknown quantities. When the horizontal stresses SHmax and Shmin are nearly the same, and they can be approximately obtained from the Poisson's ratio in the vertical X₂-X₃ plane in terms of changes in the vertical effective stress Δσ_(V) or Δσ₃₃. The steps described below can be utilized.

Given

$\begin{matrix} {{{\Delta\;\sigma_{11}} = {{\Delta\;\sigma_{22}} = {\left( \frac{v}{1 - v} \right)\Delta\;\sigma_{33}}}},} & (49) \end{matrix}$ where Δσ₁₁ and Δσ₂₂ denote the maximum and minimum horizontal stresses, an incremental change in the effective stiffness ΔC₅₅ can be expressed in terms of changes in the effective vertical stress between two depths in a reasonably uniform lithology interval

$\begin{matrix} {{{\Delta\; C_{55}} = {\left\lbrack {1 + \frac{\left( {1 - v - {2v^{2}}} \right)}{2\left( {1 - v^{2}} \right)}} \right\rbrack\left( {1 + \frac{C_{155}}{\mu}} \right)\Delta\;\sigma_{33}}},} & (50) \end{matrix}$ where C₁₅₅ is one of the three nonlinear constants referred to the chosen depth interval. An incremental change in the effective stiffness ΔC₆₆ can be expressed in terms of changes in the effective vertical stress between two depths in a reasonably uniform lithology interval

$\begin{matrix} {{{\Delta\; C_{66}} = {\left\lbrack {\frac{v}{1 - v} + {\frac{\left( {1 - v - {2v^{2}}} \right)}{2\left( {1 - v^{2}} \right)}\left( {\frac{C_{144}}{\mu} - 1} \right)}} \right\rbrack\Delta\;\sigma_{33}}},} & (51) \end{matrix}$ where C₁₄₄ is another nonlinear constants referred to the chosen depth interval. An incremental change in the effective stiffness ΔC₃₃ can be expressed in terms of changes in the effective vertical stress between two depths in a reasonably uniform lithology interval

$\begin{matrix} {{{\Delta\; C_{33}} = {\left\lbrack {1 + {\frac{\left( {1 - v - {2v^{2}}} \right)}{2\left( {1 - v^{2}} \right)}\left( {\frac{C_{111}}{\mu} - \frac{3C_{33}}{\mu}} \right)}} \right\rbrack\Delta\;\sigma_{33}}},} & (52) \end{matrix}$ where C₁₁₁ is the third nonlinear constant referred to the chosen depth interval. Equations (50), (51), and (52) are used to calculate the three nonlinear constants (C₁₁₁, C₁₄₄, C₁₅₅) in the chosen depth interval. These nonlinear constants together with linear constants enable determination of the stress coefficients of velocities in the chosen depth interval.

A second step is to use general 3D-equations relating changes in the effective stresses to corresponding changes in the effective elastic moduli and estimate the unknown stress magnitudes SHmax and Shmin in the chosen depth interval where the three nonlinear constants have been estimated. These equations are as shown below:

$\begin{matrix} {{{\Delta\; C_{55}} = {{\left\lbrack {C_{55} - {vC}_{144} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{11}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {C_{144} - {\left( {1 + {2v}} \right)C_{55}} - {2{vC}_{155}}} \right\rbrack\frac{{\Delta\sigma}_{22}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{2{\mu\left( {1 + v} \right)}} + C_{55} - {vC}_{144} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{33}}{2{\mu\left( {1 + v} \right)}}}}},} & (53) \end{matrix}$ where ΔC₅₅ is obtained from the fast-dipole shear slowness and formation bulk density at the top and bottom of the interval.

$\begin{matrix} {{{\Delta\; C_{44}} = {{\left\lbrack {{{- \left( {1 + {2v}} \right)}C_{44}} + C_{144} - {2{vC}_{155}}} \right\rbrack\frac{{\Delta\sigma}_{11}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{- {vC}_{144}} + C_{44} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{22}}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{2{\mu\left( {1 + v} \right)}} + C_{44} - {vC}_{144} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{{\Delta\sigma}_{33}}{2{\mu\left( {1 + v} \right)}}}}},} & (54) \end{matrix}$ where ΔC₄₄ is obtained from the slow-dipole shear slowness and formation bulk density at the top and bottom of the interval.

$\begin{matrix} {{{\Delta\; C_{66}} = {{\left\lbrack {{\mu\left( {1 + v} \right)} + C_{66} - {vC}_{144} + {\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{{- \left( {1 + {2v}} \right)}C_{66}} + C_{144} - {2{vC}_{155}}} \right\rbrack\frac{{\Delta\sigma}_{33}}{2{\mu\left( {1 + v} \right)}}}}},} & (55) \end{matrix}$ where ΔC₆₆ is obtained from the Stoneley shear slowness dispersion and formation bulk density at the top and bottom of the interval.

$\begin{matrix} {{{\Delta\; C_{33}} = {{\left\lbrack {\left( {1 - {2v}} \right)C_{111}} \right\rbrack\frac{\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22} + {\Delta\sigma}_{33}} \right)}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{{- \left( {1 + {2v}} \right)}C_{33}} - {4\left( {1 - v} \right)C_{155}}} \right\rbrack\frac{\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}{2{\mu\left( {1 + v} \right)}}} + {\left\lbrack {{2{\mu\left( {1 + v} \right)}} + {\left( {3 + {2v}} \right)C_{33}} + {8{vC}_{155}}} \right\rbrack\frac{{\Delta\sigma}_{33}}{2{\mu\left( {1 + v} \right)}}}}},} & (56) \end{matrix}$ where ΔC₃₃ is obtained from the compressional slowness and formation bulk density at the top and bottom of the interval. Note that the Young's modulus Y=2μ(1+v); and ΔC ₃₃=ρ_(B) V _(C,B) ²−ρ_(A) V _(C,A) ²,  (57) ΔC ₄₄=ρ_(B) V _(SS,B) ²−ρ_(A) V _(SS,A) ²,  (58) ΔC ₅₅=ρ_(B) V _(FS,B) ²−ρ_(A) V _(FS,A) ²,  (59) ΔC ₆₆=ρ_(B) V _(HS,B) ²−ρ_(A) V _(HS,A) ²,  (60) where the index A and B denote the top and bottom of the chosen depth interval.

Estimation of C₁₄₄ and C₁₅₅ in a uniform lithology interval will now be described. Assuming cross-dipole dispersions overlay implying that there is no shear wave splitting, then SHmax (σ₁₁)=Shmin (σ₂₂), and in equations (52) and (53), σ₁₁=σ₂₂. The objective is to invert the borehole Stoneley and dipole slowness data to estimate the ratio of Δσ_(V)/Δσ_(h) in a given depth interval with a reasonably uniform lithology. Over a given depth interval,

$\begin{matrix} {{{\Delta\; C_{44}} = {{\Delta\sigma}_{33} + {\left\lbrack {{{- \frac{\left( {1 + {2v}} \right)}{2\left( {1 + v} \right)}}{\Delta\sigma}_{11}} + \frac{\left( {{\Delta\sigma}_{22} + {\Delta\sigma}_{33}} \right)}{2\left( {1 + v} \right)}} \right\rbrack\frac{C_{44}}{\mu}} + {\left\lbrack {\frac{{\Delta\sigma}_{11}}{2\left( {1 + v} \right)} - {\frac{v}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{22} + {\Delta\sigma}_{33}} \right)}} \right\rbrack\frac{C_{144}}{\mu}} + {\left\lbrack {{{- \frac{v}{\left( {1 + v} \right)}}{\Delta\sigma}_{11}} + {\frac{\left( {1 - v} \right)}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{22} + {\Delta\sigma}_{33}} \right)}} \right\rbrack\frac{C_{155}}{\mu}}}},} & (61) \\ {{{\Delta\; C_{66}} = {{\frac{1}{2}\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)} + {\left\lbrack {\frac{\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}{2\left( {1 + v} \right)} - {\frac{\left( {1 + {2v}} \right)}{2\left( {1 + v} \right)}{\Delta\sigma}_{33}}} \right\rbrack\frac{C_{66}}{\mu}} + {\left\lbrack {\frac{{\Delta\sigma}_{33}}{2\left( {1 + v} \right)} - {\frac{v}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}} \right\rbrack\frac{C_{144}}{\mu}} + {\left\lbrack {{{- \frac{v}{\left( {1 + v} \right)}}{\Delta\sigma}_{33}} + {\frac{\left( {1 - v} \right)}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}} \right\rbrack\frac{C_{155}}{\mu}}}},} & (62) \end{matrix}$ It is now possible to solve for the nonlinear parameters C₁₄₄ and C₁₅₅ from the following matrix equation:

$\begin{matrix} {\mspace{79mu}{{{\begin{bmatrix} A_{11} & A_{12} \\ A_{21} & A_{22} \end{bmatrix}\begin{Bmatrix} \frac{C_{144}}{\mu} \\ \frac{C_{155}}{\mu} \end{Bmatrix}} = \begin{Bmatrix} B_{1} \\ B_{2} \end{Bmatrix}},\mspace{79mu}{where}}} & (63) \\ {\mspace{79mu}{{A_{11} = {\frac{{\Delta\sigma}_{11}}{2\left( {1 + v} \right)} - {\frac{v}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{22} + {\Delta\sigma}_{33}} \right)}}},}} & (64) \\ {\mspace{79mu}{{A_{12} = {{{- \frac{v}{\left( {1 + v} \right)}}{\Delta\sigma}_{11}} + {\frac{\left( {1 - v} \right)}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{22} + {\Delta\sigma}_{33}} \right)}}},}} & (65) \\ {\mspace{79mu}{{B_{1} = {{\Delta\; C_{44}} - {\Delta\sigma}_{33} + {\left\lbrack {{\frac{\left( {1 + {2v}} \right)}{2\left( {1 + v} \right)}{\Delta\sigma}_{11}} - \frac{\left( {{\Delta\sigma}_{22} + {\Delta\sigma}_{33}} \right)}{2\left( {1 + v} \right)}} \right\rbrack\frac{C_{44}}{\mu}}}},}} & (66) \\ {\mspace{79mu}{{A_{21} = {\frac{{\Delta\sigma}_{33}}{2\left( {1 + v} \right)} - {\frac{v}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}}},}} & (67) \\ {\mspace{79mu}{{A_{22} = {{{- \frac{v}{\left( {1 + v} \right)}}{\Delta\sigma}_{33}} + {\frac{\left( {1 - v} \right)}{2\left( {1 + v} \right)}\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}}},}} & (68) \\ {{B_{2} = {{\Delta\; C_{66}} - {\frac{1}{2}\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)} - {\left\lbrack {\frac{\left( {{\Delta\sigma}_{11} + {\Delta\sigma}_{22}} \right)}{2\left( {1 + v} \right)} - {\frac{\left( {1 + {2v}} \right)}{2\left( {1 + v} \right)}{\Delta\sigma}_{33}}} \right\rbrack\frac{C_{66}}{\mu}}}},} & (69) \end{matrix}$ Having estimated the acoustoelastic coefficient A_(E) in terms of C₁₄₄ and C₁₅₅ as described by equation (68),

$\begin{matrix} {{A_{E} = {2 + \frac{C_{155} - C_{144}}{2\mu}}},} & (68) \end{matrix}$ t is possible to estimate the ratio of the vertical to horizontal effective stresses from the equation given below:

$\begin{matrix} {{A_{E} = \frac{{\Delta\; C_{55}} - {\Delta\; C_{66}}}{{\Delta\sigma}_{V} - {\Delta\sigma}_{h}}},} & (69) \end{matrix}$ where all quantities on the RHS are estimated at a given depth. Therefore, the ratio of the vertical to horizontal effective stresses can now be calculated from the equation given below:

$\begin{matrix} {{\frac{{\Delta\sigma}_{V}}{{\Delta\sigma}_{h}} = {1 + \frac{{\Delta\; C_{55}} - {\Delta\; C_{66}}}{{\Delta\sigma}_{h}A_{e}}}},} & (70) \end{matrix}$ or equivalently,

$\begin{matrix} {{\frac{{\Delta\sigma}_{h}}{{\Delta\sigma}_{v}} = {1 - \frac{{\Delta\; C_{55}} - {\Delta\; C_{66}}}{{\Delta\sigma}_{V}A_{E}}}},} & (71) \end{matrix}$

Algorithm II is a preferred technique in environments where the formation exhibits azimuthal isotropy in cross-dipole dispersions implying that horizontal stresses are nearly the same at all azimuths. Further, this technique is more suitable for formations where lithology is rapidly changing with depth than Algorithm I. The presence of a borehole causes near-wellbore stress distributions that can be described by equations (1) through (4).

-   -   In the absence of a borehole, the far-field stresses are given         by equations (5) through (8).     -   Subtracting the far-field stresses from the near-wellbore         stresses yields incremental stresses as we approach the borehole         surface and are given by equations (9) through (12).

When the formation lithology is rapidly changing with depth, a more suitable way to invert borehole sonic data for the horizontal to overburden stress ratio may be to use radial profiles of the three shear moduli together with near-wellbore stress distributions in terms of the far-field stresses as described by Kirsch's equations (Jaeger and Cook, 1969). This procedure includes the steps described below. The effective radial and hoop stresses as a function of radial position in polar coordinates can be expressed in terms of the far-field horizontal stress and over- or under-pressure ΔP_(W)=(P_(w)−P_(P)), in the wellbore fluid using: σ_(rr)(r=2a,θ=0°)=−¼(σ_(H) +ΔP _(W)),  (72) σ_(θθ)(r=2a,θ=0°)=¼(σ_(H) +ΔP _(W)),  (73) where θ=0°, corresponds to the azimuth parallel to the maximum horizontal stress direction. Similarly, the radial and hoop stresses at r=5a, can be obtained from equations (9) through (12) and they take the form σ_(rr)(r=5a,θ=0°)=− 1/25(σ_(H) +ΔP _(W)),  (74) σ_(θθ)(r=5a,θ=0°)= 1/24(σ_(H) +ΔP _(W)),  (75)

Changes in the fast dipole shear modulus C55 at radial positions r=2a and r=5a, caused by the presence of local stresses can be expressed as ΔC ₅₅(r=2a)=¼(2C ₅₅ +C ₁₅₅ −C ₁₄₄)(1+ν)(σ_(H) +ΔP _(W)),  (76) ΔC ₅₅(r=5a)= 1/25(2C ₅₅ +C ₁₅₅ −C ₁₄₄)(1+ν)(σ_(H) +ΔP _(W)),  (77) Form a difference equation ΔC ₅₅(r=2a)−ΔC ₅₅(r=5a)=ζ(2C ₅₅ +C ₁₅₅ −C ₁₄₄)(1+ν)(σ_(H) +ΔP _(W)),  (78) where ζ=¼− 1/25=0.21. Use the following equation to calculate the left-hand-side of equation (78) ΔC ₅₅(r=2a)−ΔC ₅₅(r=5a)=ρ[V _(S) ²(r=2a)−V _(S) ²(r=5a)],  (79) where V_(S) denotes the shear velocity at different radial positions obtained from the Dipole Radial Profiling (DRP) of shear velocity. The acoustoelastic coefficient A_(E) can be written as

$\begin{matrix} {{A_{E} = {\frac{C_{55} - C_{66}}{\sigma_{V}\left( {1 - x} \right)} = {2 + \frac{C_{155} - C_{144}}{2\mu}}}},} & (80) \end{matrix}$ where μ is the far-field shear modulus in the assumed reference state. Replacing (C₁₅₅-C₁₄₄) in terms of the far-field shear modulus C₅₅ and C₆₆ from equation (80) yields, from equation (78),

$\begin{matrix} {{{\rho\left\lbrack {{V_{S}^{2}\left( {r = {2a}} \right)} - {V_{S}^{2}\left( {r = {5a}} \right)}} \right\rbrack} = {\left\lbrack {{2C_{55}} - {2{\mu\left( {\frac{C_{55} - C_{66}}{\sigma_{V} - \sigma_{H}} - 2} \right)}}} \right\rbrack\left( {1 + v} \right)\left( {\sigma_{H} + {\Delta\; P_{W}}} \right)\zeta}},} & (81) \end{matrix}$ Since the effective overburden stress is generally known, it is possible solve for the horizontal to overburden stress ratio from the following equation

$\begin{matrix} {{{\rho\left\lbrack {{V_{S}^{2}\left( {r = {2a}} \right)} - {V_{S}^{2}\left( {r = {5a}} \right)}} \right\rbrack} = {\left\lbrack {{2C_{55}} - {2{\mu\left( {\frac{C_{55} - C_{66}}{\sigma_{V}\left( {1 - x} \right)} - 2} \right)}}} \right\rbrack\left( {1 + v} \right)\left( {{x\;\sigma_{V}} + {\Delta\; P_{W}}} \right)\zeta}},} & (82) \end{matrix}$ where σ_(H)=x σ_(V), and it is possible to solve for this unknown from equation (82), which is a quadratic equation in “x”. Alternatively, it is possible to construct a cost function ε that needs to be minimized as a function of the unknown parameter “x”. This cost function ε takes the form

$\begin{matrix} {{ɛ = \frac{{\xi_{1} - {\xi_{2}(x)}}}{\xi_{1}}},} & (83) \end{matrix}$ where ξ=ρ[V _(S) ²(r=2a)−V _(S) ²(r=5a)],  (84) and

$\begin{matrix} {\xi_{2} = {\left\lbrack {{2C_{55}} - {2{\mu\left( {\frac{C_{55} - C_{66}}{\sigma_{V}\left( {1 - x} \right)} - 2} \right)}}} \right\rbrack\left( {1 + v} \right)\left( {{x\;\sigma_{V}} + {\Delta\; P_{W}}} \right){\zeta.}}} & (85) \end{matrix}$ Since the shear modulus C₆₆ is also affected by reservoir fluid mobility and overburden shale anisotropy, there is a need to compensate for these effects on the estimation of stress magnitudes using sonic data. One approach is to estimate the horizontal to overburden stress ratio as a function of parameter γ=C′₆₆/C₆₆. If the fluid mobility causes a decrease in the measured C₆₆ by 10%, then the measured C₆₆ can be increased by 10% (referred to as the corrected C′₆₆). Hence, it is possible to estimate stress magnitudes using this algorithm for γ=1.1, and this estimate is effectively compensated for fluid mobility bias on measured C₆₆.

Similarly to the approach described above, in order to estimate stress magnitudes in the overburden shale that generally exhibits transversely-isotropic (TI) anisotropy, one approach is to determine the magnitude of TI-anisotropy in terms of the ratio of C₆₆/C₄₄ from core data. If this ratio is 1.3, then the measured C₆₆ is decreased by 30% in order to remove the structural anisotropy effects from the stress magnitude estimation algorithm. Consequently, the estimate of stress magnitudes in this shale interval corresponds to the values obtained for γ=0.7.

Therefore, the parameter x is estimated for a range of C′₆₆=γ C₆₆. Finally, the ratio of the horizontal to overburden stress is given by: S _(H) /S _(V)=(xσ _(V) +αP _(P))/(σ_(V) +αP _(P)).  (86)

While the invention is described through the above exemplary embodiments, it will be understood by those of ordinary skill in the art that modification to and variation of the illustrated embodiments may be made without departing from the inventive concepts herein disclosed. Moreover, while the preferred embodiments are described in connection with various illustrative structures, one skilled in the art will recognize that the system may be embodied using a variety of specific structures. Accordingly, the invention should not be viewed as limited except by the scope and spirit of the appended claims. 

What is claimed is:
 1. A method for estimating stress ratio in a formation in which a borehole is present comprising: locating a borehole tool in the borehole of the formation, said borehole tool having at least acoustic sensor, and using the borehole tool to provide radial profiles of Stoneley slowness for the formation and dipole shear slownesses for the formation; using processing circuitry to (i) calculate at least one of dipole shear moduli C44 and C55 using the dipole shear slownesses; (ii) calculate modulus C66 using the Stoneley slowness; (iii) estimate horizontal to overburden stress ratio by inverting (i) a difference equation obtained from far-field shear modulus C66 and at least one of moduli C44 and C55, (ii) a difference equation obtained from a radial profile of at least one of dipole shear moduli C44 and C55 at two or more different radial positions within the formation, and (iii) a relationship between stresses within the formation proximate to the borehole and stresses in the far-field of the formation; and (iv) produce an indication of the horizontal to overburden stress ratio.
 2. The method of claim 1 further comprising determining that fast and slow shear dispersion curves of the formation overlay and do not exhibit a crossing signature.
 3. The method of claim 1 further comprising determining that radial profiles of dipole shear moduli C44 and C55 overlay so that C44 and C55 are equal.
 4. The method of claim 1 further comprising estimating an increase in the Stoneley shear modulus (C66) caused by the structural anisotropy in a formation containing shales as determined from measurements on core samples subject to hydrostatic pressures, and, prior to inverting, decreasing the measured C66 by the same amount to obtain the horizontal to overburden stress ratio that is compensated for intrinsic anisotropy in a formation containing shales.
 5. Apparatus for estimating stress ratio in a formation in which a borehole is present comprising: at least one acoustic sensor that provides radial profiles of Stoneley slowness for the formation and-dipole shear slownesses for the formation; processing circuitry that estimates horizontal to overburden stress ratio by inverting (i) a difference equation obtained from far-field shear modulus C66 and at least one of moduli C44 and C55 for the formation, (ii) a difference equation obtained from a radial profile of at least one of dipole shear moduli C44 and C55 at two or more different radial positions within the formation, and (iii) a relationship between stresses within the formation proximate to the borehole and stresses in the far-field of the formation; and an output that produces an indication of the horizontal to overburden stress ratio.
 6. The apparatus of claim 5 wherein the processing circuitry is operative to determine that fast and slow shear dispersion curves of the formation do not exhibit a crossing signature.
 7. The apparatus of claim 5 wherein the processing circuitry is operative to determine that radial profiles of dipole shear moduli C44 and C55 overlay so that C44 and C55 are equal.
 8. The apparatus of claim 5 wherein the processing circuitry is operative to estimate an increase in the Stoneley shear modulus (C66) caused by the structural anisotropy in a formation containing shales as determined from measurements on core samples subject to hydrostatic pressures, and, prior to inverting, decrease the measured C66 by the same amount to obtain the horizontal to overburden stress ratio that is compensated for intrinsic anisotropy in a formation containing shales.
 9. A method for estimating stress ratio in a formation in which a borehole is present comprising: locating a borehole tool in the borehole of the formation, said borehole tool having at least one acoustic sensor, and using the borehole tool to provide compressional slowness for the formation and to provide radial profiles of Stoneley slowness for the formation and dipole shear slownesses for the formation; using processing circuitry to (i) calculate compressional moduli C33 in a far-field of the formation using compressional slowness; (ii) calculate at least one of dipole shear moduli C44 and C55 in the far-field of the formation using the dipole shear slownesses; (iii) calculate modulus C66 in the far-field of the formation using the Stoneley slowness; (iv) estimate horizontal to overburden stress ratio by inverting (i) a difference equation obtained from C33 in the far-field of the formation at two different depths within an interval of the formation, (ii) a difference equation obtained from at least one of dipole shear moduli C44 and C55 in the far-field of the formation at two different depths within the interval of the formation, and (iii) a difference equation obtained from modulus C66 in the far-field of the formation at two different depths within the interval of the formation; and (v) produce an indication of the horizontal to overburden stress ratio.
 10. The method of claim 9 further comprising determining that fast and slow shear dispersion curves of the formation overlay and do not exhibit a crossing signature.
 11. The method of claim 9 further comprising determining that radial profiles of dipole shear moduli C44 and C55 overlay so that C44 and C55 are equal.
 12. Apparatus for estimating stress ratio in a formation in which a borehole is present comprising: at least one acoustic sensor that provides (i) compressional slowness for the formation and (ii) radial profiles of Stoneley slowness and dipole shear slownesses for the formation; processing circuitry that estimates horizontal to overburden stress ratio by inverting (i) a difference equation obtained from C33 in the far-field of the formation at two different depths within an interval of the formation, (ii) a difference equation obtained from at least one of dipole shear moduli C44 and C55 in the far-field of the formation at two different depths within the interval of the formation, and (iii) a difference equation obtained from modulus C66 in the far-field of the formation at two different depths within the interval of the formation; and an output that produces an indication of the horizontal to overburden stress ratio.
 13. The apparatus of claim 12 wherein the processing circuitry is operative to determine that fast and slow shear dispersion curves of the formation do not exhibit a crossing signature.
 14. The apparatus of claim 12 wherein the processing circuitry is operative to determine that radial profiles of dipole shear moduli C44 and C55 overlay so that C44 and C55 are equal. 